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Comparison of Theoretical and Experimental Steady Wing Loads on a Space Shuttle Configuration at Mach Numbers of 0.6 and 1.4
John S. Preisser
Harold E. Lowder
出版
National Aeronautics and Space Administration
, 1976
URL
http://books.google.com.hk/books?id=5oczqN27nXUC&hl=&source=gbs_api
